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| United States Patent |
5,265,457
|
|
Hayashi
, et al.
|
November 30, 1993
|
Method of forming an oil groove on the end surface of a rotor of an
aluminum alloy
Abstract
An oil groove is formed on the end surface of a rotor of an aluminum alloy
for a compressor of a vane type, in an economical manner by a method
comprising forming the oil groove of a concave type on the end surface of
the rotor slidably moving in contact with a side plate by warm-pressing a
die stamp.
| Inventors:
|
Hayashi; Tetsuya (Itami, JP);
Fujiwara; Tosio (Itami, JP)
|
| Assignee:
|
Sumitomo Electric Industries, Ltd. (Osaka, JP)
|
| Appl. No.:
|
969516 |
| Filed:
|
October 30, 1992 |
Foreign Application Priority Data
| Current U.S. Class: |
72/364; 29/888.025; 418/178 |
| Intern'l Class: |
B21K 001/28 |
| Field of Search: |
418/77,178,179
72/364,412
29/888.025
|
References Cited
U.S. Patent Documents
| 3469433 | Sep., 1969 | Fresch et al. | 72/364.
|
| 4384828 | May., 1983 | Rembold et al. | 418/178.
|
| 4689864 | Sep., 1987 | Fukuma et al. | 72/412.
|
| 4815953 | Mar., 1989 | Iio | 418/179.
|
| Foreign Patent Documents |
| 36945 | Feb., 1988 | JP | 72/412.
|
Primary Examiner: Larson; Lowell A.
Attorney, Agent or Firm: Wenderoth, Lind & Ponack
Parent Case Text
This application is a continuation of now abandoned application, Ser. No.
07/654,670, filed on Feb. 13, 1991.
Claims
What is claimed is:
1. A method of forming an oil groove on an end surface of a rotor of a high
Si Aluminum alloy having a high deformation resistance and compressing
force at normal temperature, for a compressor of a vane rotary type, which
comprises forming the oil groove of a concave type in a depth of at most
2.0 mm on the end surface of the rotor slidably moving in contact with a
side plate, by warm-pressing a die stamp on the end surface at a rotor
temperature of 200.degree. to 450.degree. C. by use of a metal die having
a protrusion whose point has a curvature radius of 0.1 to 2.0 mm and whose
side surface has a tangent angle of 30 to 75.degree. in the pressing
direction, wherein the aluminum alloy is a powder-sintered alloy or
continuously case alloy consisting of:
Si: 12 to 30% by weight
Cu: 0.5 to 5% by weight
Mg: 0.2 to 2% by weight transition element: 1 to 10% by weight
Al: balance.
Description
BACKGROUND OF THE INVENTION
1. Field of the Invention
The present invention relates to an improvement in an aluminum rotor for a
compressor of a vane rotary type, and in particular, it is concerned with
a method of forming an oil groove for preventing adhesion in a light
aluminum alloy rotor.
2. Description of the Prior Art
A rotor of a compressor used for car air conditioners has a plurality of
vane grooves through which vanes slidably move as shown in FIG. 1, and is
consolidated in one body with a rotary shaft. The rotor is revolved while
being slidably moved on the inner wall surfaces of side plates fixed to
both sides of a cylinder block. A refrigerant gas is drawn in a
compression space partitioned by five components of the rotor, vane,
cylinder block and both side plates, and is then compressed and
discharged. Since the compression space requires air-tightness it is
designed so that these components have very small clearances among them,
and in particular, when the rotor and side plates are slidably moved under
compressive force, adhesion tends to take place between them.
Up to the present time, steel materials or ferrous sintered alloys have
been used as the rotor and flake graphite cast iron or ferrous sintered
alloys have been used as the side plate. In combinations of ferrous
materials, the problem of adhesion is not serious since the materials are
relatively excellent in wear resistance and the flake graphite cast iron
or sintered alloys are excellent in oil retention. As occasion demands, an
oil groove has been provided on one side surface or both side surfaces of
a rotor to prevent such adhesion.
Of late, it has been studied to convert the material of a compressor from
ferrous materials to aluminum, with the increased necessity for realizing
a light weight compressor. Thus, it has been rendered possible to make a
rotor of aluminum, for which aluminum could not be used up to the present
time, by development of a powdered aluminum alloy consisting of a quenched
and solidified powder and a high strength aluminum material, with the
progress of the continuous casting technique. As to the side plate, the
conversion of the material thereof into aluminum has also been possible by
the use of high silicon aluminum materials such as A 390 material
(commercial name). These alloys are not sufficient in adhesion resistance
between the rotor and side plate in spite of the fact that large amounts
of alloying components such as Si, etc. are contained therein so as to
improve the wear resistance and adhesion resistance and to maintain the
clearance precision at a high level. In particular, since adhesion tends
to readily occur in a case where oil is exhausted on the sliding surface,
an oil groove is necessary at the end surface of the rotor.
Since in the case of a rotor of an aluminum alloy, it is impossible to form
an oil groove during powder compacting as in the case of the prior art
rotors of sintered ferrous materials, because of the restriction on the
production method, a step of working the oil groove should nevertheless be
newly added. As the working method, an end mill or discharge working can
be taken into consideration, but these methods have a problem that the
installation thereof is of high rank and the working cost is too high.
Furthermore, in the end mill working, the degree of freedom for imparting
a groove shape is small.
SUMMARY OF THE INVENTION
It is an object of the invention to provide a method of making a rotor of
an aluminum alloy whereby the above described problems can be solved.
It is another object of the present invention to provide a method of making
a rotor of an aluminum alloy for a compressor of a vane rotary type,
provided with an oil groove on the end surface of the rotor in an
economical manner.
These objects can be attained by a method of forming an oil groove on the
end surface of a rotor of an aluminum alloy for a compressor of a vane
rotary type, which comprises forming the oil groove of a concave type on
the end surface of the rotor slidably moving in contact with a side plate
by warm-pressing a die stamp.
BRIEF DESCRIPTION OF THE DRAWINGS
The accompanying drawings illustrate the principle and merits of the
invention.
FIG. 1 is a schematic view of a rotor for a compressor of a vane rotary
type,
FIG. 2 (A) and FIG. 3 (A) are respectively cross-sectional views of metal
dies used for pressing and forming oil grooves as shown in FIG. 1, and
FIGS. 2 (B) and FIG. 3 (B) are schematic views of the shapes of the oil
grooves respectively obtained by the above described metal dies.
DETAILED DESCRIPTION OF THE INVENTION
The present invention provides a method of forming an oil groove of a rotor
of an aluminum alloy in a simple and economical manner, which comprises
warm-pressing a die stamp to form a concave groove on the end surface of
the rotor which is to slidably move with a side plate.
In a preferred embodiment of the present invention, the aluminum alloy
contains 12 to 30% by weight of silicon since it is required that the
aluminum alloy, as a material of the rotor as described above, has a lower
coefficient of thermal expansion, higher wear resistance and higher Youngs
modulus in order to maintain stable clearance with high precision between
the rotor and other parts, and if necessary, the aluminum alloy contains
0.5 to 5.0% by weight of Cu and 0.2 to 2.0 by weight of Mg, as aging and
hardening elements for increasing the strength and hardness. As occasion
demands, transition elements such as Fe, Ni, Mn, etc. are incorporated in
a proportion of 1.0 to 10.0% by weight so as to improve heat resistance,
wear resistance and mechanical properties.
Preferably, pressing the die is ordinarily carried out at a temperature of
150 to 450.degree. C. to soften the rotor itself, and the metal die for
forming an oil groove, used during the same time, has such a protrusion
that its point shape R is in the range of 0.1 to 2.0 mm and the tangent
angle on the side surface of the protrusion is in the range of 30.degree.
to 75.degree.. The depth of the oil groove is generally at most 2.0 mm.
FIG. 2 (A) and FIG. 3 (A) are respectively cross-sectional views of
examples of metal dies used for pressing and forming oil grooves as shown
in FIG. 1, and FIG. 2 (B) and FIG. 3 (B) are schematic views of the oil
grooves obtained by the above described metal dies. In FIG. 2 (A), the
curvature radius R and the tangent angle .theta. of the side surface of
the protrusion are shown to represent the point shape of the protrusion of
the metal die.
The above described composition of an aluminum alloy, as a material of a
rotor suitable for the present invention, will be illustrated hereinafter.
The aluminum alloy can be any of powder-sintered alloys and alloys made by
continuous casting.
Si as a predominant additive element is effective for lowering the
expansion coefficient and improving the wear resistance and toughness by
increasing the content thereof. If the content of Si is less than 12% by
weight, the coefficient of thermal expansion is high and the wear
resistance is not sufficient, while if more than 30% by weight, the
ductility is deteriorated and the notch toughness of the rotor is lowered.
Thus, the content of Si should be in the range of 12.0 wt % to 30.0 wt %.
Furthermore, when the content of Si is less than 12% by weight,
workability of the material is large and accordingly, it is not necessary
to effect warm-pressing a die stamp as one feature of the present
invention. When exceeding 30% by weight, the ductility of the material is
lowered so that cracking tends to take place by pressing a die stamp. From
this point of view, it is also preferred that the content of Si is in the
range of from 12.0% by weight to 30% by weight.
Cu and Mg are age-hardening elements for increasing the strength and
hardness of alloys. If the content of Cu is less than 0.5% or that of Mg
is less than 0.2% it is impossible to obtain a sufficient strength and
hardness. If the content of Cu is more than 5% or that of Mg is more than
2% by weight, coarse precipitates are formed to rather deteriorate the
strength and lower the heat stability. Therefore, it is desired that the
content of Cu is in the range of 0.5 to 5.0% by weight and that of Mg is
in the range of 0.2 to 2.0% by weight.
In order to improve the heat resistance, wear resistance and mechanical
properties, if necessary, transition elements such as Fe, Ni, Mn, etc. are
incorporated in the alloy. If the contents thereof are less than 1.0% by
weight, the additive effects are small, while if more than 10.0% by
weight, the toughness of the material is lowered, the reliability of the
material is decreased and the workability is lowered so that cracking
tends to take place by pressing a die stamp. Thus, the transition elements
are preferably incorporated in a proportion of 1.0 to 10.0% by weight.
When an oil groove is formed in a rotor having the above described
composition, cold-pressing a die stamp results in cleavage or cracking
because of large amounts of transition elements and Si serving to lower
the ductility of the material.
Accordingly, it is required to effect the pressing of the die stamp under
such a state that the material is heated and softened. The heating
temperature depends on the composition of the material and the shape of
the oil groove, but the rotor itself is preferably heated at 150.degree.
to 450.degree. C. during pressing a die stamp. If the temperature is lower
than 150.degree. C., cleavage or cracking tends to occur and the
deformation resistance is so large that a high compressing force is
required. When exceeding 450.degree. C., the material is annealed and
precipitated or crystallized materials such as Si crystals become coarser
than required, which deteriorates the quality of the material, while in
addition, the related installation is of a higher cost. Therefore, the
heating temperature of the rotor itself during pressing a die is
preferably 150.degree. to 450.degree. C.
Limitation of the range in the protrusion shape of a metal die will now be
illustrated. Since the rotor material contains large amounts of transition
elements or Si serving to lower the ductility as described, cleavage or
cracking tends to take place even in the case of warm-pressing a die. In
particular, if the point shape R of the protrusion is less than 0.1 mm,
cleavage or cracking tends to occur, while if the point R exceeds 2.0 mm,
a large pressing force is required when it is desired to maintain a
sufficient depth of the oil groove so that the quantity of deformation in
the vertical direction to the pressing direction is large and the vicinity
of the vane groove of the rotor is deformed to narrow the width of the
vane groove and to lower the dimensional precision. Thus, it is desired
that the point shape R of the protrusion of the metal mold is in the range
of 0.1 to 2.0 mm.
When the tangent angle at the side surface of the protrusion of the metal
mold is less than 30.degree., the rise toward the end surface of the rotor
is so large that chamfering takes place between the end part of the
protrusion and the rotor material. When larger than 75.degree., a similar
problem arises to the case where the point shape R is large. Thus, it is
desired that the tangent angle of the protrusion of the metal die is in
the range of 30.degree. to 75.degree. in the pressing direction.
The depth of the oil groove obtained by pressing a metal die is ordinarily
at most 2.0 mm, since if more than 2.0 mm, cleavage or cracking tends to
take place and the material is removed toward the end surface or the
vicinity of the vane grooves by plastic deformation to hardly obtain
dimensional precision.
As illustrated above, according to the present invention, the oil groove
can be formed on the rotor end surface of an aluminum alloy of a
compressor by warm-pressing a die to form a concave groove part using a
simple pressing apparatus with a simple operation, a low cost and a high
yield of material.
EXAMPLES
Using 15 powder-sintered aluminum alloys and 2 continuous casting aluminum
alloys as the rotor material, experiments were carried out with varying
the pressing and forming conditions, thus obtaining results as shown in
Table 1, in which Sample Nos. 1 to 21 were powder-sintered alloys and
Sample Nos. 22 to 29 were continuous casting alloys. In Table 1, the
results were assessed by marks, .circleincircle.: very good, o: good, x:
not good.
TABLE 1
Results of Pressing and Forming Experiments Maximum Maximum
Alloy Composition Shape of Die Protrusion Groove Deformation Deformatio
n Occurrence Sample of Rotor (wt %) Temperature Point Tangent Die Load
Depth after in Length of Vane of Cleavage No. Si Cu Mg Fe Ni Mn
(.degree.C.) Shape R (mm) angle .theta..degree. (Ton) Forming (mm)
Direction (mm) Groove (mm) and Cracking Judgement
1 8 4.1 0.6 <0.3 <0.1 0.3 300 as shown 0.8 60 5.0 1.4 0.05 0.06
.circleincircle. in FIG. 2(A) 2 12 4.0 0.5 <0.3 <0.1 0.3
5.0 1.0 0.03 0.04 .circleincircle. 3 20 3.6 0.5 <0.3 <0.1 0.3 5.0
0.9 0.03 0.04 .circleincircle. 4 30 3.2 0.4 <0.3 <0.1 0.2 5.0 0.7
0.03 0.05 .smallcircle. 5 35 2.9 0.4 <0.3 <0.1 0.2 5.0 0.6 0.03
0.04 yes x
6 20 1.0 0.2 <0.3 <0.1 0.3 5.0 1.0 0.04 0.05 .circleincircle. 7
20 4.5 1.6 <0.3 <0.1 0.3 4.2 1.1 0.05 0.05 .smallcircle. 8 20 5.8
3.0 <0.3 <0.1 0.3 4.0 1.1 0.05 0.05 yes x 9 17 3.0 1.0 2.0 <0.1
0.5 5.8 0.8 0.04 0.05 .circleincircle. 10 17 3.0 1.0 7.0 <0.1 0.5
6.1 0.7 0.03 0.04 .smallcircle. 11 17 3.0 1.0 12.0 <0.1 0.5
8.8 0.8 0.06 0.05 yes x 12 17 3.0 1.0 <0.3 5.0 0.5 5.6 0.8 0.03
0.05 .circleincircle. 13 17 3.0 1.0 <0.3 <0.1 5.0 5.6 0.9 0.03
0.05 .circleincircle. 14 17 3.0 1.0 5.0 <0.1 0.4 100 0.8 60 14.5
0.9 0.04 0.07 yes x 15 17 3.0 1.0 5.0 <0.1 0.4 200 8.3 1.0 0.04
0.07 .smallcircle. 16 17 3.0 1.0 5.0 <0.1 0.4 350 4.0 1.2 0.05
0.10 .circleincircle. 17 17 3.0 1.0 5.0 <0.1 0.4 500 1.1 1.5 0.10
0.25 expanded x 18 20 0.2 <0.4 4.2 1.6 <0.1 400 FIG. 2(A) 0.05 60
3.0 1.8 0.10 0.02 yes x 19 20 0.2 <0.4 4.2 1.6 <0.1 0.5 4.0 1.2
0.06 0.03 .circleincircle. 20 20 0.2 <0.4 4.2 1.6 <0.1 1.5 4.7
0.7 0.04 0.04 .circleincircle. 21 20 0.2 <0.4 4.2 1.6 <0.1 3.0
5.0 0.4 0.02 0.03 x 22 20 1.2 1.2 0.5 0.1 0.5 300 FIG. 2(A) 0.8 25
2.3 0.7 0.10 0.02 yes x 23 20 1.2 1.2 0.5 0.1 0.5 40 2.9 0.7 0.06
0.03 .smallcircle. 24 20 1.2 1.2 0.5 0.1 0.5 70 3.4 0.6 0.04 0.04
.circleincircle. 25 20 1.2 1.2 0.5 0.1 0.5 80 3.7 0.6 0.02 0.03
x 26 17 4.2 1.5 0.5 0.1 0.5 250 FIG. 3(A) 2.7 0.4 0.02 0.02
.circleincircle. 27 17 4.2 1.5 0.5 0.1 0.5 3.3 0.8 0.04 0.03
.circleincircle. 28 17 4.2 1.5 0.5 0.1 0.5 4.0 1.6 0.06 0.04
.smallcircle. 29 17 4.2 1.5 0.5 0.1 0.5 5.3 2.4 0.10 0.07 yes
x
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